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词条 Didier Pti'tAvion
释义

  1. Design and development

  2. Specifications (Pti'tAvion)

  3. References

  4. External links

name=Pti'tAvion image= caption=

}}{{Infobox Aircraft Type

type=Ultralight aircraft national origin=France manufacturer=Didier ULM designer= first flight= introduced= retired= status=In production primary user= more users= produced= number built= program cost= unit cost= €33,290 (assembled, 2015) developed from= variants with their own articles=
}}

The Didier Pti'tAvion ({{lang-en|Small Airplane}}) is a French ultralight aircraft that was designed and produced by Didier ULM of Francheval. The aircraft is supplied as a kit for amateur construction or as a complete ready-to-fly-aircraft.[1][2][3]

Design and development

The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a strut-braced high-wing a two-seats-in-side-by-side configuration enclosed cockpit, fixed tricycle landing gear and a single engine in tractor configuration.[1][2][3]

The aircraft is made predominantly from welded steel tubing, with its flying surfaces covered in doped aircraft fabric. Its {{convert|9.40|m|ft|1|abbr=on}} span wing, has an area of {{convert|15.04|m2|sqft|abbr=on}} and it constructed using a welded steel tube lattice spar, aluminium tube ribs and a laminate leading edge. The standard engine is the {{convert|80|hp|kW|0|abbr=on}} Rotax 912UL four-stroke powerplant. The cockpit is {{convert|1.15|m|in|1|abbr=on}} wide and is intended to accommodate "bulky crew".[1][2][3]

The aircraft comes with its own open-frame trailer for ground transport.[1][2][3]

Specifications (Pti'tAvion)

{{Aircraft specs
|ref=Bayerl[1]
|prime units?=met


|genhide=
|crew=one
|capacity=one passenger
|length m=
|length ft=
|length in=
|length note=
|span m=9.40
|span ft=
|span in=
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=15.04
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=275
|empty weight lb=
|empty weight note=
|gross weight kg=450
|gross weight lb=
|gross weight note=
|fuel capacity={{convert|53|l}}
|more general=


|eng1 number=1
|eng1 name=Rotax 912UL
|eng1 type=four cylinder, liquid and air-cooled, four stroke aircraft engine
|eng1 kw=60
|eng1 hp=
|prop blade number=3
|prop name=composite
|prop dia m=
|prop dia ft=
|prop dia in=
|prop note=


|perfhide=
|max speed kmh=175
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=150
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=65
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|range km=
|range miles=
|range nmi=
|range note=
|endurance=
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=5
|climb rate ftmin=
|climb rate note=
|time to altitude=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}

References

1. ^Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 40. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
2. ^Bertrand, Noel; Rene Coulon; et al: World Directory of Leisure Aviation 2003-04, page 135. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485X
3. ^Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 75. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}

External links

  • {{Official website|http://www.ptitavion.com/}}

3 : French ultralight aircraft 2000–2009|Homebuilt aircraft|Single-engined tractor aircraft

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